[fltsim.0] title=OV-10E BRONCO sim=OV-10A_BRONCO model= panel=Custom sound= texture= kb_checklists= kb_reference= atc_id_color=0xffffffffff atc_id=0194 ui_manufacturer=North American ui_type=OV-10E BRONCO ui_variation=Fuerza Aérea Venezolana visual_damage=1 description=El North American Rockwell OV-10A\\\/E Bronco, es utilizado por la Fuerza Aérea Venezolana en tareas de reconocimiento y patrullaje en las zonas fronterizas y Costeras de nuestro Territorio.\n\nRepaint by Daniel Borrego atc_heavy=0 atc_airline=Fuerza Aérea Venezolana atc_flight_number=FAV [fltsim.1] title=FAC Bronco sim=OV-10A_BRONCO model= panel=Custom sound= texture=custom kb_checklists= kb_reference= atc_id_color=0xffffffffff atc_id=0194 ui_manufacturer=North American ui_type=OV-10E BRONCO ui_variation=VietNam FAC visual_damage=1 description=North American Rockwell OV-10A\\\/E Bronco atc_heavy=0 atc_airline=Air Force atc_flight_number=AF682 [General] atc_type=NAMC atc_model=OV10 editable=1 performance=Envergadura: 12.19m (40 ft)\nLargo: 12.67m (41 ft 65 in)\nAlto: 4.62 m (15 ft 1 in) \nMotor: 2 Garrett T76-G-410\/411 turboprop \nVelocidad Máxima 452 km\/h\s 281 mph \nVelocidad Mínima 204 km\/h\s 110 kts\s 127 mph \nRata de ascenso 2,800 ft\/min (853 m\/min) \nTecho 9,144 m\s 30,000 ft \n\nArmamento: 2 ametralladoras M60 de 7.62-mm, 500 rondas cada una. 1,200-lb (544-kg) de capacidad en 4 puntos en el fuselaje, 2 puntos sobre las alas para 100-gal (378-l) en tanques tipo gotera, pods de cañones, rockets, bombas, misiles aire-aire.\n\nAvion de: Tim Piglet Conrad\nTexturas de: Edaurdo Fadul eduardofadul@yahoo.com \nhttp:\/\/usuarios.lycos.es\/fuerzaaereacolombia\/ [WEIGHT_AND_BALANCE] max_gross_weight= 9908.000 empty_weight= 6969.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, 5.000, 0.000, 0.000 station_load.1= 170.000, 5.000, 2.000, 0.000 station_load.2= 170.000, -2.100, -2.000, 0.000 station_load.3= 170.000, -2.100, 2.000, 0.000 station_load.4= 170.000, -5.300, -2.000, 0.000 station_load.5= 170.000, -5.300, 2.000, 0.000 ;Moments of Inertia empty_weight_pitch_MOI= 30000.000 empty_weight_roll_MOI= 18200.000 empty_weight_yaw_MOI= 36500.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type= 5 Engine.0= 3.773, -7.467, 0.000 Engine.1= 3.773, 7.467, 0.000 fuel_flow_scalar= 1.000 min_throttle_limit=-0.250000 [propeller] thrust_scalar=1 propeller_type= 0 propeller_diameter= 9.000 propeller_blades= 3 propeller_moi= 24.000 beta_max= 45.000 beta_min= 15.200 min_gov_rpm= 25520.000 prop_tc= 0.004 gear_reduction_ratio= 17.600 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 700.000 beta_feather= 79.300 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 rotation=2,-1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW [TurbineEngineData] fuel_flow_gain= 0.011 inlet_area= 1.000 rated_N2_rpm= 29920.000 static_thrust= 75.000 afterburner_available= 0 [turboprop_engine] power_scalar=.75 maximum_torque= 3270.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 -light_panel=0, 5 , 17.0+ //0 Class <0=none,1=wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0= 1.000, 9.724, 0.000, -5.810, 3181.000, 0.000, 0.900, 90.000, 0.296, 2.500, 0.952, 5.800, 6.800, 0.000, 0.000, 0.000 point.1= 1.000, -1.780, -7.624, -6.878, 3574.000, 1.000, 1.250, 0.000, 0.642, 2.500, 0.815, 5.500, 7.500, 2.000, 0.000, 0.000 point.2= 1.000, -1.780, 7.624, -6.878, 3574.000, 2.000, 1.250, 0.000, 0.642, 2.500, 0.815, 5.300, 7.300, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -19.777, 0.998, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, 0.000, 19.777, 0.998, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -18.952, 0.000, 0.046, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 2.500, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -1.000 static_cg_height= 4.300 gear_system_type=0 [Views] eyepoint=0, 0, 0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 1.079, -20.374, 1.564, fx_navred , light.1=3, 1.079, 20.374, 1.564, fx_navgre , light.2=1, -19.895, -7.01, 6.992, fx_beacon , light.3=1, 4.836, 0.00, -2.817, fx_beacon , light.4=4, 3.770, 0.00, .039, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= 0.000, -6.000, 1.000, 129.000, 0.000 RightMain= 0.000, 6.000, 1.000, 129.000, 0.000 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 291.000 wing_span= 40.000 wing_root_chord= 7.500 wing_dihedral= 0.000 wing_incidence= 1.000 wing_twist= -1.500 oswald_efficiency_factor= 0.700 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 1.500 htail_area= 70.000 htail_span= 14.000 htail_pos_lon= -21.500 htail_pos_vert= 7.200 htail_incidence= 0.500 htail_sweep= 0.000 vtail_area= 64.000 vtail_span= 8.000 vtail_sweep= 0.000 vtail_pos_lon= -20.500 vtail_pos_vert= 4.100 elevator_area= 22.750 aileron_area= 16.250 rudder_area= 24.000 elevator_up_limit= 17.000 elevator_down_limit= 18.000 aileron_up_limit= 18.000 aileron_down_limit= 18.000 rudder_limit= 30.000 elevator_trim_limit= 15.000 spoiler_limit= 90.000 spoilerons_available= 1 aileron_to_spoileron_gain= 4.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 96.000 full_flaps_stall_speed= 76.800 cruise_speed= 200.000 max_indicated_speed=400.000000 max_mach=0.579980 [autopilot] use_no_default_bank=1 use_no_default_pitch=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 45.000, 0.000 [SMOKESYSTEM] smoke.0=0.00,0.70, 8.00, fx_gun04 smoke.1=0.00,0.70, 7.00, fx_gun04 smoke.2=0.00,0.70, -7.00, fx_gun04 smoke.3=0.00,0.70, -8.00, fx_gun04 [fltsim.1] title=Bronco Update sim=OV-10A_BRONCO model= panel=Custom sound= texture= kb_checklists= kb_reference= atc_id_color=0xffffffffff atc_id=0194 ui_manufacturer=North American Rockwell ui_type=OV-10E BRONCO ui_variation=OV-10 Custom panel visual_damage=1 description=test panel to upgrade the poor panel for the OV-10 atc_heavy=0 atc_airline=Fuerza Aérea Venezolana atc_flight_number=FAV [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0